US9468951B2ActiveUtilityPatentIndex 63
Surface cleaning unmanned aerial vehicle
Est. expiryAug 20, 2034(~8.1 yrs left)· nominal 20-yr term from priority
Inventors:CHIN HON WAHGROSS WILLIAMHYDE RODERICK AKARE JORDIN TMYHRVOLD NATHAN PPETROSKI ROBERT CTEGREENE CLARENCE TWOOD JR LOWELL L
B64U 2201/202B64U 2201/00B08B 1/165B08B 1/16A47L 1/02E04G 23/00B08B 5/02B08B 3/02B64C 2201/027B08B 1/00B64C 2201/024B08B 1/002B64C 2201/14E04G 23/002H02G 1/02B64C 2201/148B64C 39/024B64U 2101/29B64U 30/299B64U 50/34Y02E10/50G05D 1/0094B08B 1/12
63
PatentIndex Score
2
Cited by
16
References
15
Claims
Abstract
Described embodiments include an unmanned aerial vehicle and a method. The unmanned aerial vehicle includes an airframe and a rotary wing system coupled with the airframe and configured to aerodynamically lift the vehicle in the air. The unmanned aerial vehicle includes a flight controller configured to control a movement of the vehicle while airborne. The unmanned aerial vehicle includes a cleansing controller configured to manage a removal of a surface contaminant from a selected portion of a surface of an external object using an airflow generated by the rotary wing system.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1. An unmanned aerial vehicle comprising:
a rotary wing system configured to aerodynamically lift the vehicle in the air;
a flight controller configured to control a movement of the vehicle while airborne;
a surface contaminant sensor configured to measure a contamination state of a surface; and
a cleansing controller configured to manage a removal of a surface contaminant from a selected portion of a surface of an external object using an airflow generated by the rotary wing system and based on data acquired by the surface contaminant sensor;
wherein measuring the contamination state of the surface occurs prior to an initial removal of the surface contaminant; and
wherein the cleansing controller is configured to:
determine an airflow force sufficient to dislodge the surface contaminant;
direct only a portion of a total airflow generated by the rotary wing system at the selected portion of the surface based on the determined airflow force; and
select the direction of the portion of the airflow based on data from the surface contaminant sensor.
2. The vehicle of claim 1 , wherein the surface contaminant sensor is configured to measure a size or characteristic of particles located on a portion of the surface of the external object.
3. The vehicle of claim 1 , wherein the surface contaminant sensor includes an optical sensor.
4. The vehicle of claim 1 , wherein the surface contaminant sensor includes an ultrasound sensor.
5. The vehicle of claim 1 , wherein the surface contaminant sensor includes a polarized light source and an optical sensor configured to detect at least one of a presence or an amount of diffuse reflection of polarized light by the surface, the polarized light first emitted by the polarized light source.
6. The vehicle of claim 1 , wherein the flight controller is responsive to an instruction from the cleansing controller to direct at least a portion of the airflow generated by the rotary wing system at a selected portion of the surface with sufficient force to dislodge the surface contaminant.
7. The vehicle of claim 1 , wherein the flight controller is configured to control a cleaning route of the vehicle relative to the selected portion of the surface in response to a record of a previous cleaning activity.
8. The vehicle of claim 1 , wherein the flight controller controls a cleaning route taken by the unmanned aerial vehicle based on a characteristic of the surface contaminant measured by the surface contaminant sensor.
9. The vehicle of claim 1 , wherein the rotary wing system includes a helicopter, quad-copter, or quad-rotor configuration.
10. The vehicle of claim 1 , wherein the rotary wing system includes a protective structure to decrease any damage caused by a contact between the rotary wing system and the external object.
11. The vehicle of claim 1 , wherein the rotary wing system includes a duct which partially surrounds at least a portion of the rotary wing system.
12. The vehicle of claim 1 , wherein the external object includes a solar panel.
13. The vehicle of claim 1 , wherein the external object includes an exterior window of a building or other stationary structure.
14. The vehicle of claim 1 , wherein the external object includes a component of an electrical power transmission line.
15. The vehicle of claim 1 , wherein the external object includes a mirror or an array of mirrors.Cited by (0)
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